Eldorado International (Bogota)

IATA/ICAO CODE: BOG/SKBO
CITY: Bogota
COUNTRY: Colombia

AIRPORT CONTACT

No changes reported by the airport in 2011
Verify information below with the airport


Name: Sede Corporativa OPAIN S.A.
Aeropuerto Internacional El Dorado
Title: Commutador General
Airport: El Dorado International Airport
Address:

Aeropuerto Internacional El Dorado
Bogota, D.C. Colombia
Phone: +571 425 1000 - 413 8702 or 413 8284
Fax: +571 413 8586
Email: +571 413 5104
Airport Web Site: www.aerocivil.gov.co

ELEVATION: 8358 ft.
RUNWAY INFORMATION
Orientation
Length (m)
Displaced
Threshold (m)
Glide Slope(deg)
Width (m)
13L/31R
3800
-
-
45
13R/31L
3800
-
-
45

NOISE ABATEMENT PROCEDURES

Runway 13 L/R
This procedure implies a reduction of power at a prescribed minimum altitude and delay the flaps/slats retraction until a maximum prescribed altitude is reached. At the prescribed altitude, accelerate and retract flaps/slats maintaining a positive rate of climb and completing the transition to en-route normal climbing procedures.

- The climb speed until noise abatement starting point will not be less than V2+10 kts.

- Left turn: Reaching 800 ft AGL or R NDB, turn LEFT, adjust and maintain engine power. Maintain a climbing speed of V2+10kts with flaps and slats in take-off configuration.

- RIGHT turn: Maintain runway heading until 036 degrees bearing from TEH NDB and start turn. Reaching 800 ft AGL and adjust and maintain the engine power according to the noise reduction flaps and slats in takeoff configuration.

- At 11,000 ft, maintaining a positive rate of climb, accelerate and retract flaps/slats.

- At 12,500 ft accelerate to en-route climb speed.

Note 1: Maintain maximum climb gradient in the initial takeoff phase.
Note 2: For DC-10 aircraft the criteria will be V2+20 kts.
Note 3: Reduced takeoff power procedure is recommended in accordance with the operational manual.

In addition, the following criteria should be taken into account:

1. The power rules to be applied after the failure or loss of one engine, or any other apparent loss of performance, at any stage of takeoff or climb during the noise abatement procedure, will be at pilot in command discretion, and noise abatement considerations will no longer apply.

2. The maximum acceptable angle for each kind of fuselage will not be exceeded.

Runway 31 L/R
This procedure implies a reduction of power at a prescribed minimum altitude and delay the flaps/slats retraction until a maximum prescribed altitude is reached. At the prescribed altitude, accelerate and retract flaps/slats maintaining a positive rate of climb and completing the transition to en-route normal climbing procedures.

- The climb speed until noise abatement starting point will not be less than V2+10kts.
- Reaching 400 ft AGL start turn. At 800 ft AGL adjust and maintain climb engine power. Maintain a climbing speed of V2+10kts with flaps and slats in take-off configuration.

- At 11,000 ft , maintaining a positive rate of climb, accelerate and retract flaps/slats.

- At 12,500 ft, accelerate to en-route climb speed.

Note 1: Maintain maximum climb gradient in the initial take-off phase.
Note 2: Fro DC10 aircraft the criteria will be V2+20kts.
Note 3: Reduced take-off power procedure is recommended in accordance with the operational manual.

In addition, the following criteria should be taken into account:

1. The power rules to be applied after the failure or loss of one engine, or any other apparent loss of performance, at any stage of takeoff or climb during the noise abatement procedure, will be at pilot in command discretion, and noise abatement considerations will no longer apply.

2. The maximum acceptable angle for each kind of fuselage will not be exceeded.

CONTINUOUS DESCENT ARRIVAL (CDA) - NONE

AIRPORT CURFEWS - NONE

PREFERENTIAL RUNWAYS - NONE

OPERATING QUOTA - NONE

ENGINE RUN-UP RESTRICTIONS - NONE

APU OPERATING RESTRICTIONS - NONE

NOISE BUDGET RESTRICTIONS - NONE

NOISE SURCHARGE - NONE

NOISE MITIGATION/LAND USE PLANNING PROGRAM INFORMATION
Type of Program
Date Implemented
Status
Sound Insulation (Residences and Public Buildings)
-
-
Purchase Assurance for Homeowners Located Within the Airport Noise Contours
-
-
Avigation Easements
-
-
Zoning Laws
-
-
Real Estate/Property Disclosure Laws
-
-
Acquire Land for Noise Compatibility to date
-
-
Population within each noise contour level relative to aircraft operations
-

-

Airport Noise Contour Overlay Maps
-
-
Total Cost of Noise Mitigation Programs to Date
-

-

Source of Noise Mitigation Program Funding for Aircraft Noise
-
-

NOISE MONITORING SYSTEM - NONE

FLIGHT TRACK MONITORING SYSTEM - NONE

NOISE LEVEL LIMITS - NONE

CHAPTER 2 RESTRICTIONS
See Chapter 2 Phase out below.

CHAPTER 2 PHASEOUT
The phase out of Chapter 2 aircraft in Colombia was completed as of January 1, 2003.

CHAPTER 3 RESTRICTIONS - NONE